Tribology in Engineering 2013
DOI: 10.5772/50795
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High Speed Rotors on Gas Bearings: Design and Experimental Characterization

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Cited by 6 publications
(4 citation statements)
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“…It is also reported that GFBs can operate even at a high speed of 500 kr/min. 3,4 In 1994, Heshmat 5 achieved a breakthrough maximum pressure of 6.735 bar at 59.7 kr/min rotational speed while designing foil bearings. The use of gas bearings in the field of turbomachinery led several researchers to propose different types of foil bearings to improve load-carrying capacity.…”
Section: Introductionmentioning
confidence: 99%
“…It is also reported that GFBs can operate even at a high speed of 500 kr/min. 3,4 In 1994, Heshmat 5 achieved a breakthrough maximum pressure of 6.735 bar at 59.7 kr/min rotational speed while designing foil bearings. The use of gas bearings in the field of turbomachinery led several researchers to propose different types of foil bearings to improve load-carrying capacity.…”
Section: Introductionmentioning
confidence: 99%
“…The exceptional advantages of aerostatic bearings are the high rotation speed and extremely low friction [1][2][3][4][5]. The bearings are lubricated with compressed gas from the source into the flow path, which usually uses passive elements to limit the gas flow to create a certain pressure which is necessary to maintain the current load and to control the displacement of the moving part of the structure, thereby ensuring its stiffness [4][5][6][7][8][9][10][11][12][13][14][15][16]. And although the development of technology has contributed to the improvement of bearings, they still have a drawback-low stiffness [8,10,17,18].…”
Section: Introductionmentioning
confidence: 99%
“…However, the evolving design of the gas foil bearings (GFBs) has improved the dynamic characteristics of the gas bearings, enhancing its scope of application. The GFBs are capable of operating at a speed over 500 krpm [3,4]. Gas foil journal bearings (GFJBs) and gas foil thrust bearings (GFTBs) are used to bear radial loads and axial loads, respectively, developed in the rotor of the turboexpander.…”
Section: Introductionmentioning
confidence: 99%